NTSB CAROL · Event
Event ERA24LA057
Registry · N53AA
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2016 · 7 years old at event
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20160910
ADS-B equipped
Yes — Mode-S A6AE15
Registrant of record
MUSTANG SALLY AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
An encounter with a downdraft while maneuvering at low altitude, which resulted in a collision with a fence.
Factual narrative
According to the flight instructor, he was simulating an engine failure with the student pilot. He selected a field to approach and proceeded to reduce the engine rpm to simulate the engine failure. They continued the maneuver until they were approximately 100 feet above the ground, at which point he instructed the student pilot to add full power and climb out. The student pilot complied, but right at that moment, the flight instructor felt a heavy gust of wind. He described it as a downdraft, and despite the engine producing full power, it would not climb. The flight instructor took control of the airplane and attempted to recover it from the descent. The airplane continued to descended until it collided with a fence and touched down in the field. During the landing roll, the airplane impacted a tree, resulting in substantial damage to the horizontal stabilizer. The pilots reported that there were no pre-accident mechanical malfunctions or failures with the airplane that would have precluded normal operation. An engine test run was facilitated, and no anomalies were noted during the test. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Environmental issues-Conditions/weather/phenomena-Wind-Downdraft-Effect on operation
- — Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Ability to respond/compensate
Verbatim from NTSB's published report. Source file
NTSB_2023_ERA24LA057.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
Browse the full corpus — academia portal ↗